fighter aircraft

Simulation of a Fault Diagnosis Method for Air Cycle System of Fighter Aircraft

战斗机空气循环系统故障诊断方法的仿真研究

Design of detection & evaluation ground system for fighter aircraft maneuverability

某型歼击机操纵性能地面检测评估系统设计

A method of developing load spectrum for a fighter aircraft

歼击机载荷谱编制方法的研究

The algorithm has been used successfully in fighter aircraft vulnerability analysis .

该算法可以有效地应用于飞机易损性分析计算中。

On Design Loads for New - Generation Fighter Aircraft

关于新一代飞机的设计载荷

Design and Estimation of Pilot Operation Procedure for Fighter Aircraft

战斗机飞行员操作程序的设计和评估

Study on Nonlinear H_ ∞ Guidance Law for Fighter Aircraft Pursuit

战机追踪非线性H∞导引律研究

The Design of Robust Feedback Controller for a Fighter Aircraft

歼击机的鲁棒反馈控制器设计

Dynamic Evaluation of Fighter Aircraft Effectiveness in Air-Combat Based on HLA Simulation

基于HLA仿真的空战动态效能评估研究

A Preliminary Study of Effectiveness of Fighter Aircraft Intercepting Cruise Missile

歼击机拦截巡航导弹效能的初步研究

Air-combat ability and sensitivity analysis of modern fighter aircraft

现代战斗机空战能力评估及敏感性分析

Application of Quaternion in fighter aircraft flight simulation

四元数在战斗机飞行仿真中的应用

Estimation of Air Combat Effectiveness for Fighter Aircraft

战斗机空战效能评估

An Algorithm for Fast Recognizing the Numerals on Fighter Aircraft Gauge Board

一种快速识别飞机仪表参数的算法

Investigation into Super-Maneuverability and Associated Tactical Superiority for High Performance Fighter Aircraft

超机动性技术及其战术优势探讨

A New Algorithm of Multi-Shadowed Projective Area and Its Application in Fighter Aircraft Vulnerability Analysis

军机易损性分析中多重遮挡投影面积计算

New technique , new airborne equipment and weapon for increasing combat capability of fighter aircraft are described .

文章概述了为提高歼击机作战能力所采用的新技术和新的机载武器。

Many of the current fighter aircraft use maneuvering flaps to enhance air combat maneuverability .

机动襟翼是现代战斗机提高机动格斗能力的常用措施。

The circuitry in this fighter aircraft has been protected against strong magnetic fields .

这架战斗机里的电路系统受到保护，不受强磁场影响。

Some Researches on Key Techniques When a Fighter Aircraft is Modified with an Active Radar Guided Missile

歼击机配装主动雷达制导导弹关键技术研究

Design of an Adaptive Control Augmentation Stability System for Fighter Aircraft Whose Flight Altitude and Mach Number Vary

飞机在变高度和变马赫数下自适应控制增稳系统的设计

The aircraft may be a technology demonstrator or a prototype for a mass production fighter aircraft .

这架飞机也许是技术验证机或者大规模生产型号的原型机。

The closer coast would allow the covering fighter aircraft to fuel and return in shorter time .

较近的海岸可以缩短作掩护的战斗机加油和返航的时间。

Review of airframe / inlet integration of maneuver fighter aircraft

论机动飞机机体/进气道一体化

Development of Integrated Environmental Control System / Thermal Management System ( IECS / TMS ) for Next Generation Fighter Aircraft

下一代战斗机综合环境控制/热管理系统开发现状

Air to air active radar guided missile is the most important air combat weapon for modern fighter aircraft .

主动雷达制导型空空导弹是当今战斗飞机最重要的空战武器。

The estimation method is applicable to third-and fourth-generation fighter aircraft .

公式是着眼于第三代/第四代飞机起飞总重估算建立的，当然适用于该类飞机起飞总重的估算。

A series of simulations , such as fighter aircraft , etc. , show the effectiveness of the proposed methods .

歼击机神经网络自适应重构控制等一系列数字仿真结果表明了本文方法的有效性。

The flexibility in display size and the diversity of data are not available in any other fighter aircraft .

显示尺寸的灵活性和显示数据的多样性在其它任何作战飞机上都不曾有过。

The results of the study have certain referential value to the development of the fourth generation and other advanced fighter aircraft .

研究结果对四代机等先进战斗机的风洞试验技术发展具有一定的参考价值。